Navier Stokes with chemical reaction

Click For Summary
SUMMARY

This discussion focuses on integrating chemical reactions into the Navier-Stokes equations, particularly in the context of combustion processes in jet engines. Key considerations include calculating the enthalpy of combustion, understanding the relationship between reaction rates and thermodynamic properties like pressure and density, and utilizing scalar fields for reaction rates and temperature. Additionally, the discussion touches on the chemical composition of kerosene and its classification, emphasizing the need for accurate data on its constituents and enthalpy values.

PREREQUISITES
  • Understanding of Navier-Stokes equations
  • Knowledge of thermodynamics, specifically enthalpy and reaction kinetics
  • Familiarity with combustion chemistry and fuel properties
  • Experience with scalar fields in fluid dynamics
NEXT STEPS
  • Research methods for incorporating chemical reactions into Navier-Stokes equations
  • Study the thermodynamic properties of kerosene and its combustion characteristics
  • Explore computational fluid dynamics (CFD) tools for simulating combustion processes
  • Investigate existing literature on coupled Navier-Stokes equations for multi-species flows
USEFUL FOR

Researchers, engineers, and students in fluid dynamics, combustion science, and aerospace engineering who are looking to deepen their understanding of chemical reactions in fluid flow systems.

optrix
Messages
33
Reaction score
0
I wasn't sure whether to put this in Aerospace, but decided on physics in the end.

1.) How do you factor a chemical reaction into the solution for the Navier Stokes equations? More precisely, how can you include the affects of a heat absorbing (endothermic), or heat releasing (exothermic) chemical reaction going in within the flow field? The main thing I have in mind is combustion reactions that occur in jet engines, which are of course exothermic.

My thoughts were that you would first have to calculate the enthalpy of combustion of the fuel. Then the amount of heat being released is related to the reaction rate, which depends on pressure, and density of air/fuel at a given point (Maybe even "concentration" is a better word). But then in turn, the amount of heat being released would affect the thermal expansion of the gas, and hence the pressure at that point, which again would change the reaction rate and amount of heat being released...etc... until maybe it reaches some kind of equilibrium?

I was also thinking that you would have to use scalar fields of the form f(x,t) for reaction rate and temperature. Would this be accurate?

2.) A related question - kerosene is made up of a whole mixture of hydrocarbons, and other things.

i. where can I find a list of the exact chemical compostion of kerosene? (I believe it may come in different 'grades' or classes, like A1, A2.)

ii. can you consider kerosene to be a uniform mixture of its constituent compounds, and therefore asign to it an overall enthalpy of combustion, which is like an average for all the constituents?


I'm having a lot of trouble finding information on any of these things, so if anyone knows then please help me out. (Number 1 is the main concern, but though I might as well drop number 2 in there too :) )

Appreciate any help, regards, Joe
 
Science news on Phys.org
Can't help with number 1 but Kerosene is also called No. 1 distillate. During the refining of crude oil the fraction obtained after gasoline is a light distillate called kerosene.

The API gravity for No. 1 oil is between 40 and 44. this is a low sulfur oil with about 135,000 btu's per gallon. The carbon and hydrogen content of 40 API gravity oil is

Specific gravity: .8251

% carbon: 85.93

% Hydrogen: 13.07

% noncombustibles: 1
 
For part 1, the energy absorbed/released would be applied in the heat source of the energy equation. The continuity equation would have to account for the destruction of the fuel and oxidizer and the creation of combustion species, and similar for the momentum equation.

I've not done NS for combustion systems however.
 
You will have many coupled N-S type equations:

1) the conservation of mass, for each species, including sources and sinks via the chemical reactions
2) the conservation of momentum equations for each species, including diffusion via concentration gradients in the body force term.
3) the conservation of energy equations for each species, taking into account the thermodynamics of all the chemical reactions.

There should be some simplifications out there- I worked with combustion folks in the past- but I forget the details.
 

Similar threads

Replies
20
Views
6K
  • · Replies 4 ·
Replies
4
Views
6K
  • · Replies 3 ·
Replies
3
Views
3K
  • · Replies 12 ·
Replies
12
Views
3K
  • · Replies 4 ·
Replies
4
Views
2K
  • · Replies 18 ·
Replies
18
Views
2K
  • · Replies 53 ·
2
Replies
53
Views
5K
  • · Replies 46 ·
2
Replies
46
Views
6K
  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 2 ·
Replies
2
Views
2K